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Rauzy, A. ) IMBSA 2014. LNCS, vol. 8822, pp. 181– 194. fi Abstract. Satellite formation flying is an example of an autonomous distributed system that relies on complex coordinated mode transitions to accomplish its mission. While the technology promises significant economical and scientific benefits, it also poses a major verification challenge since testing the system on the ground is impossible. In this paper, we experiment with formal modelling and proof-based verification to derive mode logic for autonomous flight formation.

Since there are no other means to restore the coordination, failure to restore coordination by the ground control implies failure of the entire mission. This observation implies our next requirement: R5. In the MANUAL mode in the perigee phase the ground control should control both the Leader and the Follower to restore coordination between them. Upon successful completion of this, the control is passed to the Leader and a transition to an active mode PARKING or OPERATIONAL becomes enabled. Communication is a critical aspect in ensuring coordination and safety of the autonomous formation flying.

Battery part is composed of two Hot Buses, which are used to interface the Batteries (BATT1 and BATT2). The batteries are powered by the Hot Buses through the Emergency Buses connected to them, or the batteries source the Emergency Buses through the Hot Buses temporarily, until the RAT deploys and takes on the powering task. The HiP-HOPS method was applied in the electrical system case study following all the guidelines. The steps applying the method will not be herein described due to space limitations.

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